RU2545558C2 - Задний узел гондолы турбореактивного двигателя - Google Patents

Задний узел гондолы турбореактивного двигателя Download PDF

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RU2545558C2
RU2545558C2 RU2012127242/11A RU2012127242A RU2545558C2 RU 2545558 C2 RU2545558 C2 RU 2545558C2 RU 2012127242/11 A RU2012127242/11 A RU 2012127242/11A RU 2012127242 A RU2012127242 A RU 2012127242A RU 2545558 C2 RU2545558 C2 RU 2545558C2
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Russia
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RU2012127242/11A
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Russian (ru)
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RU2012127242A (ru
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Ги Бернар ВОШЕЛЬ
Пьер КАРЮЭЛЬ
Жан-Филипп ЖОРЕ
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Эрсель
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/08—Inspection panels for power plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243—Flange connections; Bolting arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
RU2012127242/11A 2009-12-07 2010-11-26 Задний узел гондолы турбореактивного двигателя RU2545558C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR09/05903 2009-12-07
FR0905903A FR2953490B1 (fr) 2009-12-07 2009-12-07 Ensemble arriere de nacelle pour turboreacteur
PCT/FR2010/052546 WO2011070266A1 (fr) 2009-12-07 2010-11-26 Ensemble arrière de nacelle pour turboréacteur

Publications (2)

Publication Number Publication Date
RU2012127242A RU2012127242A (ru) 2014-01-20
RU2545558C2 true RU2545558C2 (ru) 2015-04-10

Family

ID=42313777

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2012127242/11A RU2545558C2 (ru) 2009-12-07 2010-11-26 Задний узел гондолы турбореактивного двигателя

Country Status (9)

Country Link
US (1) US20120247571A1 (pt)
EP (1) EP2509870B1 (pt)
CN (1) CN102648128A (pt)
BR (1) BR112012012078A2 (pt)
CA (1) CA2780299A1 (pt)
ES (1) ES2503562T3 (pt)
FR (1) FR2953490B1 (pt)
RU (1) RU2545558C2 (pt)
WO (1) WO2011070266A1 (pt)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2999239B1 (fr) * 2012-12-12 2015-02-20 Aircelle Sa Inverseur de poussee de nacelle et nacelle equipee d'au moins un inverseur
WO2014164238A1 (en) 2013-03-13 2014-10-09 United Technologies Corporation Gas turbine engine hydraulically operated nacelle latch
US9404507B2 (en) * 2013-04-15 2016-08-02 Mra Systems, Inc. Inner cowl structure for aircraft turbine engine
FR3009339B1 (fr) * 2013-07-30 2018-01-26 Safran Aircraft Engines Turbomachine comprenant un dispositif de refroidissement du pylone
US9915225B2 (en) 2015-02-06 2018-03-13 United Technologies Corporation Propulsion system arrangement for turbofan gas turbine engine
FR3047522B1 (fr) 2016-02-04 2018-03-16 Safran Aircraft Engines Ensemble propulsif pour aeronef
US11781506B2 (en) 2020-06-03 2023-10-10 Rtx Corporation Splitter and guide vane arrangement for gas turbine engines
RU2745276C1 (ru) * 2020-06-03 2021-03-23 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Капот газогенератора турбореактивного двигателя

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3541794A (en) * 1969-04-23 1970-11-24 Gen Electric Bifurcated fan duct thrust reverser
RU13201U1 (ru) * 1999-08-04 2000-03-27 Запорожское машиностроительное конструкторское бюро "Прогресс" им.акад.А.Г.Ивченко Устройство для технического обслуживания газотурбинного двигателя с реверсором тяги в вентиляторном контуре
EP1174341A1 (fr) * 2000-07-17 2002-01-23 Hurel-Hispano Meudon Perfectionnements aux arrière-corps de nacelle, à tuyère commune, de réaction d'avions
FR2916426A1 (fr) * 2007-05-22 2008-11-28 Aircelle Sa Ensemble arriere de nacelle pour turboreacteur.

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3511055A (en) * 1968-05-29 1970-05-12 Rohr Corp Thrust reverser
US3779010A (en) * 1972-08-17 1973-12-18 Gen Electric Combined thrust reversing and throat varying mechanism for a gas turbine engine
US3831376A (en) * 1973-02-05 1974-08-27 Boeing Co Thrust reverser
US4679750A (en) * 1984-06-20 1987-07-14 The Boeing Company Latch system
US4998409A (en) * 1989-09-25 1991-03-12 Rohr Industries, Inc. Thrust reverser torque ring
DE19702083C1 (de) * 1997-01-22 1998-06-10 Eurocopter Deutschland Türsystem, insbesondere für ein Passagierflugzeug
GB9723022D0 (en) * 1997-11-01 1998-01-07 Rolls Royce Plc Gas turbine apparatus
US7484356B1 (en) * 2005-07-26 2009-02-03 Aeronautical Concepts Of Exhaust, Llc Cascade reverser without blocker doors
FR2907759B1 (fr) * 2006-10-31 2008-12-12 Aircelle Sa Nacelle pour turboreacteur a ouverture laterale
FR2914020B1 (fr) * 2007-03-23 2009-04-24 Airbus France Sas Procede pour reduire les emissions sonores a l'arriere d'un turbomoteur et turbomoteur perfectionne par le procede
FR2925607B1 (fr) * 2007-12-21 2013-05-10 Aircelle Sa Nacelle pour moteur d'aeronef a tuyere de section variable
FR2938878B1 (fr) * 2008-11-26 2013-11-08 Aircelle Sa Inverseur de poussee pour nacelle de turboreacteur a double flux
FR2960855A1 (fr) * 2010-06-03 2011-12-09 Aircelle Sa Nacelle pour turboreacteur avec dispositif de reprise d'efforts circonferentiels

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3541794A (en) * 1969-04-23 1970-11-24 Gen Electric Bifurcated fan duct thrust reverser
RU13201U1 (ru) * 1999-08-04 2000-03-27 Запорожское машиностроительное конструкторское бюро "Прогресс" им.акад.А.Г.Ивченко Устройство для технического обслуживания газотурбинного двигателя с реверсором тяги в вентиляторном контуре
EP1174341A1 (fr) * 2000-07-17 2002-01-23 Hurel-Hispano Meudon Perfectionnements aux arrière-corps de nacelle, à tuyère commune, de réaction d'avions
FR2916426A1 (fr) * 2007-05-22 2008-11-28 Aircelle Sa Ensemble arriere de nacelle pour turboreacteur.

Also Published As

Publication number Publication date
CA2780299A1 (fr) 2011-06-16
CN102648128A (zh) 2012-08-22
US20120247571A1 (en) 2012-10-04
BR112012012078A2 (pt) 2016-05-17
RU2012127242A (ru) 2014-01-20
WO2011070266A1 (fr) 2011-06-16
FR2953490A1 (fr) 2011-06-10
FR2953490B1 (fr) 2012-02-24
ES2503562T3 (es) 2014-10-07
EP2509870A1 (fr) 2012-10-17
EP2509870B1 (fr) 2014-06-18

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20161127